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DOI Prefix: 10.47001/IRJIET

Fatigue and Damage Tolerance Analysis on Center Wing N-XXX Aircraft Using Software

Djoeli SatrijoMechanical Engineering, Faculty of Engineering, Diponegoro University, Jl. Prof. Sudharto, SH., Tembalang-Semarang 50275, IndonesiaOjo KurdiMechanical Engineering, Faculty of Engineering, Diponegoro University, Jl. Prof. Sudharto, SH., Tembalang-Semarang 50275, IndonesiaToni PrahastoMechanical Engineering, Faculty of Engineering, Diponegoro University, Jl. Prof. Sudharto, SH., Tembalang-Semarang 50275, IndonesiaSabrina Rizky MulyanaMechanical Engineering, Faculty of Engineering, Diponegoro University, Jl. Prof. Sudharto, SH., Tembalang-Semarang 50275, IndonesiaIan YuliantiPhysics Study Program, Universitas Negeri Semarang, Central Java, Indonesia

Vol 8 No 11 (2024): Volume 8, Issue 11, November 2024 | Pages: 122-127

International Research Journal of Innovations in Engineering and Technology

OPEN ACCESS | Research Article | Published Date: 14-11-2024

doi Logo doi.org/10.47001/IRJIET/2024.811011

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Abstract

The aircraft wing is the most important part of the aircraft which functions to provide a lift so that the aircraft can fly. The material structure of the aircraft wing will experience fatigue due to its condition in the air which requires elasticity to produce continuous movement. Therefore, fatigue and damage tolerance analysis were carried out. Fatigue analysis can determine the life of a component undergoing loading from an aircraft structure, while damage tolerance analysis can predict the rate of crack propagation and the residual life of structures that have been cracked. By combining these two analyses, the best management program for aircraft structures, especially aircraft wings, can be created. In this test, calculations and analysis were performed with software with the crack growth principle. In this study, the calculation results are still within the range that should be set by the company.

Keywords

Aircraft Wing, Fatigue Analysis, Fracture Mechanic


Citation of this Article

            

Djoeli Satrijo, Ojo Kurdi, Toni Prahasto, Sabrina Rizky Mulyana, & Ian Yulianti. (2024). Fatigue and Damage Tolerance Analysis on Center Wing N-XXX Aircraft Using Software. International Research Journal of Innovations in Engineering and Technology - IRJIET, 8(11), 122-127. Article DOI https://doi.org/10.47001/IRJIET/2024.811011

Licence Copyright (c) 2026 International Research Journal of Innovations in Engineering and Technology creative common licence This work is licensed under Creative common Attribution Non Commercial 4.0 Internation Licence
References
  1. Richard, H.A. and Sander, M. (2016) ‘Fundamentals of fracture mechanics’, Solid Mechanics and its Applications, 227(October), pp. 55–112. Available at: https://doi.org/10.1007/978-3-319-32534-7_3.
  2. Cano, A.J., Salazar, A. and Rodríguez, J. (2024) ‘Structural integrity of polymers processed by additive manufacturing techniques using residual strength diagrams’, Theoretical and Applied Fracture Mechanics, 134(PB), p. 104727. Available at: https://doi.org/10.1016/j.tafmec.2024.104727.
  3. Rita Zuana Qomariyah, S.Si, M.T. (2018) ‘Dapat Memperbaiki Sistem Pemeliharaan Struktur Pesawat Udara’, Jurnal Pendiidkan, 3(2), pp. 12–16.
  4. Karimah, A.L. et al. (2022) ‘Analisis Kegagalan Material Pada Sayap Pesawat Terbang (Review)’, Jumantara Jurnal Manajemen dan Teknologi Rekayasa, 1(1), p. 26. Available at: https://doi.org/10.28989/jumantara.v1i1.1266.
  5. Yu, X. (2014) ‘On the fatigue crack growth analysis of spliced aircraft wing panels under sequential axial and shear loads’, Engineering Fracture Mechanics, 123, pp. 116–125. Available at: https://doi.org/10.1016/j.engfracmech.2014.03.018
  6. Zerbst, U., Madia, M. and Vormwald, M. (2017) ‘Fatigue strength and fracture mechanics’, Procedia Structural Integrity, 5, pp. 745–752. Available at: https://doi.org/10.1016/j.prostr.2017.07.165.
  7. Wei, Y. et al. (2024) ‘On impact response and damage tolerance of adhesively bonded joints - An experimental and numerical study’, Thin-Walled Structures, p. 112606. Available at: https://doi.org/10.1016/j.tws.2024.112606.
  8. Minigher, P. et al. (2024) ‘On an efficient global/local stochastic methodology for accurate stress analysis, failure prediction and damage tolerance of laminated composites’, International Journal of Solids and Structures, 303(January), p. 113026. Available at: https://doi.org/10.1016/j.ijsolstr.2024.113026
  9. Zhang, Y. et al. (2025) ‘Predicting the fatigue life of T800 carbon fiber composite structural component based on fatigue experiments of unidirectional laminates’, International Journal of Fatigue, 190(September 2024), p. 108622. Available at: https://doi.org/10.1016/j.ijfatigue.2024.108622.
  10. Randy Septiawan,  dan (2018) ‘Jurnal Rekayasa Material, Manufaktur dan Energi Analisa Pengujian Lelah Material Stainless Steel 304 Dengan Menggunakan Rotary Bending Fatigue Machine’, Jurnal Rekayasa Material, Manufaktur dan Energi, 1(1), pp. 64–73. Available at: https://creativecommons.org/licenses/by-sa/4.0/
  11. Richard, H.A. and Sander, M. (2016) ‘Fundamentals of fracture mechanics’, Solid Mechanics and its Applications, 227(October), pp. 55–112. Available at: https://doi.org/10.1007/978-3-319-32534-7_3.
  12. Kolditz, L.M. et al. (2024) ‘Employing Williams ’ series for the identification of fracture mechanics parameters from phase-field simulations’, Engineering Fracture Mechanics, 307(October 2023), p. 110298. Available at: https://doi.org/10.1016/j.engfracmech.2024.110298.
  13. Boutelidja, R. et al. (2024) ‘A dual fracture mechanical approach for estimating notch stress intensity factor and T-stress using volumetric methods on API 5L pipe steel: Experimental study and numerical validation’, Journal of Materials Research and Technology, 33(October), pp. 3189–3204. Available at: https://doi.org/10.1016/j.jmrt.2024.09.224.
  14. Steinfelder, C., Rempel, D. and Brosius, A. (2024) ‘Influence of the material properties on the clinching process and the resulting load-bearing capacity of the joint’, Journal of Advanced Joining Processes, 10 (February), p. 100263. Available at: https://doi.org/10.1016/j.jajp.2024.100263.
  15. Valikhani, M. et al. (2024) ‘Bayesian finite element model inversion of offshore wind turbine structures for joint parameter-load estimation’, Ocean Engineering, 313(P3), p. 119458. Available at: https://doi.org/10.1016/j.oceaneng.2024.119458.

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